What was found
LOWER FUSELAGE FRAME 86, BETWEEN STR 27R AND STR 28R WITH CORROSION. DAMAGE HAS BEEN REPORTED AND MANAGED UNDER NON ROUTINE ITEM A1D208,1-88. SHEAR TIE WAS REPLACED UNDER DWG, PN 170-65180-447, INSTRUCTIONS.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LOWER FUSELAGE FRAME 86, BETWEEN STR 27R AND STR 28R WITH CORROSION. DAMAGE HAS BEEN REPORTED AND MANAGED UNDER NON ROUTINE ITEM A1D208,1-88. SHEAR TIE WAS REPLACED UNDER DWG, PN 170-65180-447, INSTRUCTIONS.